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United States Patent |
5,142,290
|
DuFort
|
August 25, 1992
|
Wideband shaped beam antenna
Abstract
A wideband shaped beam antenna having steep beam edge slopes in one plane
is disclosed. An optical multiple beam antenna such as a geodesic lens
antenna, a Luneberg lens or a circular folded pillbox, is coupled at
selected points to a feed system having a power divider and phasing
control. Coupling of the feed system to the optical multiple beam antenna
is effected with a power transition having a wide frequency bandwidth and
a capability of conducting high power levels. To shape the beam further,
selected beams may be amplitude weighted. An aperture control device such
as an E-plane sectoral horn, is attached when required, to narrow the
beamwidth in the E-plane. By overlapping multiple beams of the optical
multiple beam antenna in accordance with the invention, a sector beam
having a constant position and constant steep edge slopes over an octave
frequency bandwidth is obtained.
Inventors:
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DuFort; Edward C. (Fullerton, CA)
|
Assignee:
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Hughes Aircraft Company (Los Angeles, CA)
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Appl. No.:
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552645 |
Filed:
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November 17, 1983 |
Current U.S. Class: |
342/372; 343/911L |
Intern'l Class: |
H01Q 003/22; H01Q 003/24; H01Q 003/26 |
Field of Search: |
343/911 L,780,773,754,368,372
|
References Cited
U.S. Patent Documents
3343171 | Sep., 1967 | Goodman, Jr. | 343/754.
|
3656165 | Apr., 1972 | Walter et al. | 343/754.
|
3680123 | Jul., 1972 | Bryant et al.
| |
3680140 | Jul., 1972 | Chalfin et al. | 343/754.
|
3754270 | Aug., 1973 | Thies, Jr. | 343/773.
|
4114162 | Sep., 1978 | Wild | 343/754.
|
4146895 | Mar., 1979 | Wild | 343/754.
|
4255751 | Mar., 1981 | Goodman, Jr. | 343/754.
|
4268831 | May., 1981 | Valentino et al. | 343/754.
|
4359738 | Nov., 1982 | Lewis | 343/754.
|
4359741 | Nov., 1982 | Cassel | 343/754.
|
4488156 | Dec., 1984 | DuFort et al. | 343/754.
|
Other References
"The Geodesic Luneberg Lens" by Richard C. Johnson, The Microwave Journal,
Aug., 1962, pp. 76-85.
"A Solution of the Problem of Rapid Scanning for Radar Antennae" by R. F.
Rinehart, Journal of Applied Physics, vol. 19, Sep., 1948 pp. 860-862.
|
Primary Examiner: Blum; Theodore M.
Attorney, Agent or Firm: Denson-Low; Wanda K.
Claims
What is claimed is:
1. An antenna system or providing a frequency independent shaped sector
beam in space, comprising:
a multiple beam antenna having multiple feed points, each of which forms a
corresponding frequency independent beam in space, the feed points being
selected so that the beams overlap to form said sector beam;
dividing means for dividing a signal into a plurality of feed signals,
predetermined ones of which are selected such that one particular feed
signal feeds one of the feed points;
phase means for selectively controlling the relative phase of the
predetermined ones of the feed signals to result in a predetermined ripple
between adjacent beams; and
transition means for simultaneously applying the predetermined ones of the
feed signals to the respective feed points.
2. The antenna system according to claim 1 wherein said feed points are
spaced from each other by one-half wavelength.
3. The antenna system according to claim 1 further comprising aperture
means for controlling the beamwidth of the beams in the plane orthogonal
to the plane of the multiple beams.
4. The antenna system according to claim 1 further comprising amplitude
means for amplitude weighting selected feed signals of said plurality of
feed signals.
5. The antenna system according to claim 1 wherein said multiple beam
antenna is selected from the group consisting of geodesic lens antennas
and Luneberg lens antennas.
6. The antenna system according to claim 1 wherein said multiple beam
antenna is selected from the group consisting of circular folded pillbox
antennas, constant dielectric lens antennas and trash can scanner
antennas.
7. The antenna system according to claim 5 further comprising aperture
means for controlling the beamwidth of the beams in the plane orthogonal
to the plane of the multiple beams.
8. The antenna system according to claim 7 wherein said aperture means
comprises a sectoral horn coupled to the multiple beam antenna.
9. The antenna system according to claim 7 wherein said transition means
comprises a shorted coaxial probe transition which couples the feed signal
to the feed point.
10. The antenna system according to claim 9 wherein said transition means
further comprises transformer means for transforming the impedance of the
shorted coaxial probe to the impedance of the multiple beam antenna at the
feed point.
11. The antenna system according to claim 10 wherein said transformer means
comprises a stepped impedance transformer disposed in the multiple beam
antenna.
12. The antenna system according to claim 9 wherein said transition means
further comprises a high impedance device coupled to said shorted coaxial
probe.
13. The antenna system according to claim 6 further comprising aperture
means or controlling the beamwidth of the beams in the plane orthogonal to
the plane of the multiple beams.
14. The antenna system according to claim 13 wherein said aperture means
comprises a sectoral horn coupled to the multiple beam antenna.
15. The antenna system according to claim 5 further comprising amplitude
means for amplitude weighting selected feed signals of said plurality of
feed signals.
16. The antenna system according to claim 6 further comprising amplitude
means for amplitude weighting selected feed signals of said plurality of
feed signals.
17. An antenna system for providing a frequency independent shaped sector
beam in space, comprising:
a multiple beam antenna having multiple feed points, each of which forms a
corresponding frequency independent beam in space, the feed points being
selected so that the beams overlap to form the sector beam;
a feed apparatus coupled to the multiple beam antenna for feeding a
plurality of feed signals to and from the multiple beam antenna,
comprising:
i) signal divider/combiner means for dividing a single signal into a
plurality of feed signals, predetermined ones of which are selected such
that one particular feed signal feeds one of the feed points, and for
combining the feed signals into a single signal;
ii) phasing control means for controlling the relative phase of the
predetermined ones of the feed signals to result in a predetermined ripple
between adjacent beams;
iii) transition means for simultaneously applying the predetermined ones of
the feed signals to the respective feed points; and
iv) aperture control means for controlling the beamwidth of the beams in
the plane orthogonal to the plane of the multiple beams.
18. The antenna system according to claim 17 wherein the multiple beam
antenna comprises a perfectly focussing multiple beam antenna.
19. The antenna system according to claim 18 wherein said perfectly
focussing multiple beam antenna is selected from the group consisting of
geodesic lens antennas and Luneberg lens antennas.
20. The antenna system according to claim 19 wherein said transition means
comprises a shorted coaxial probe transition which couples the feed signal
to the feed point.
21. The antenna system according to claim 18 wherein said aperture control
means comprises a sectoral horn coupled to the perfectly focussing
multiple beam antenna.
22. The antenna system according to claim 17 wherein the multiple beam
antenna comprises an imperfectly focussing multiple beam antenna.
23. The antenna system according to claim 22 wherein the imperfectly
focussing multiple beam antenna is selected from the group consisting of
circular folded pillbox antennas, constant dielectric lens antennas and
trash can scanner antennas.
24. The antenna system according to claim 23 wherein said aperture control
means comprises a sectoral horn coupled to the imperfectly focussing
multiple beam antenna.
25. An antenna system for providing a shaped frequency independent sector
beam in space, comprising:
a geodesic lens antenna having spacing between its conducting surfaces of
no greater than one-half wavelength whereby only the TEM mode is
propagated, said geodesic lens antenna having a plurality of feed points
disposed on its focal curve in selected positions for simultaneously
forming multiple overlapping beams in space to form said frequency
independent sector beam;
a feed apparatus coupled to said geodesic lens antenna for feeding a
plurality of signals to and from the geodesic lens antenna, comprising;
i) signal divider/combiner means for dividing a single signal into a
plurality of feed signals, predetermined ones of which are selected such
that a particular feed signal feeds one of the feed points and for
combining the feed signals into a single signal;
ii) phasing control means coupled to the predetermined ones of the feed
signals for controlling the relative phase of the predetermined ones of
the feed signals to result in a predetermined ripple between adjacent
beams;
iii) transition means for coupling the predetermined ones of the feed
signals to said respective feed points on the focal curve of the geodesic
lens antenna, said transition means comprising a coaxial shorted probe
disposed between the conducting plates of said geodesic lens antenna; and
iv) aperture control means coupled to the geodesic lens antenna for
controlling the beamwidth of the beams in the plane orthogonal to the
plane of the multiple overlapping beams, comprising a sectoral waveguide
horn.
Description
BACKGROUND OF THE INVENTION
The invention relates to shaped beam antennas and in particular, to an
antenna for forming a sector beam, the shape and position of which are
constant over a wide frequency bandwidth.
Shaped beam antennas are useful for many purposes, one of which is
efficient energy management. These antennas are becoming more useful in
other areas as the sophistication of radar systems increases. The
capabilities of precision direction finding and resolution of complex
targets where only limited scanning time is available are becoming more
and more necessary in view of the speeds and radar capabilities of modern
threats. For example, one defense against a radar equipped threat is to
steer it off target. However, the effectiveness of signals transmitted to
steer the threat off target can depend upon multipath propagation effects
which alter the transmitted beam. Multipath propagation can cause
fluctuation of 10 to 20 dB, which may distort the antenna beam to a point
where it becomes ineffective. The multipath effect becomes a significant
consideration in relation to threats which fly low to the ground or water,
or close to other stationary clutter.
Multipath fluctuations can be reduced significantly by employing shaped
beam antennas which provide steep beam slope or cut off characteristics
near the clutter position. For example, where the antenna is located on a
ship, a steep beam slope in the elevation plane near the water would be
desirable in relation to low flying threats.
In addition, since the frequency or frequencies of the radar system of the
threat are typically unknown, a wide frequency bandwidth in the shaped
beam antenna is also desirable. Coupling a wide frequency bandwidth with a
constantly shaped beam where the beam position and shape are independent
of frequency over the wide frequency bandwidth would result in an antenna
well adapted for use in high multipath environments.
The principles of geometric optics have been the design basis for prior
shaped beam antennas. One prior optical technique involves the offset feed
parabolic antenna. A point source whose radiation pattern is known
illuminates a reflector shaped such that the feed energy is redistributed
into the desired far field shape. These reflectors may also be shaped to
provide a narrow beam in the orthogonal plane. This technique is described
in more detail in Silver, Microwave Antenna Theory and Design,
McGraw-Hill, NY, 1949, pg. 497 et seq. The advantage of this technique is
simplicity and low cost. However, the feed pattern is a function of the
product of the wave number k=(2.pi./.lambda.) and the sine of the angle
.theta., so the beam position and shape in the far field vary with
frequency as k sin .theta..
In order to retain a constant far field pattern, a constant feed pattern
would be required and this is difficult to obtain. If a nonfocal feed were
used, for example an array on a spherical cap, the feed would be
broadband, however points on the feed generally would not produce focused
pencil beams in the far field, and sharp beam edges would not be obtained.
A prior optical technique is radiating directly from a spherical surface.
This produces constant beamwidth and constant beam shape over a wide
frequency bandwidth, however, again the sharp beam edges have not been
obtained.
The above described techniques are based on providing a single beam and
shaping that beam as required. Another prior technique involves a
constrained approach such as using a corporate or series type transmission
line or a waveguide power divider to feed a planar or linear aperture,
such as in the Butler beam forming array. Any realizable far field pattern
can be produced using this technique and if the Woodward synthesis is
used, the aperture size will be small and the edge shape will be the
steepest possible corresponding to the aperture size. However, in this
approach, the aperture distribution is constant with frequency, therefore
the far field pattern shape will vary as k sin .theta.. Also in this
technique, operating over too wide a frequency band changes the beamwidth,
shifts the location of the beams and can introduce grating lobes just as
with any array antenna. In particular, the beamwidth will typically be
broadened by a factor of two over a frequency bandwidth of an octave.
A variant of the above described constrained approach is given in U.S. Pat.
No. 4,146,896 to Wild (1979), where a spherical cap feeds a planar array.
As discussed above, the use of a planar array causes a narrow frequency
bandwidth for the structure. Also the beams are not fixed in position and
will vary with frequency. In order to obtain a steep beam slope plus a
one-half octave or greater frequency bandwidth, the antenna would need an
aperture of several hundred wavelengths, which is an impracticable
structure in most cases.
SUMMARY OF THE INVENTION
It is a purpose of the invention to overcome most, if not all, of the above
described problems of prior techniques by providing an antenna having a
sector beam which remains constant in shape and position over a wide
frequency band and which has steep edge slopes.
It is another purpose of the invention to provide a shaped beam antenna
capable of conducting relatively high power levels.
It is another purpose of the invention to provide an antenna which is
relatively small in size, simple in construction, light in weight and of
low manufacturing cost.
The invention accomplishes the aforementioned purposes and other purposes
by providing a wide frequency bandwidth antenna system having an optical
multiple beam antenna with an antenna feed system having a power divider,
phasing control and a wide frequency band power transition from the
phasing control to the optical multiple beam antenna and, where required,
an aperture control to narrow the beamwidths.
In the invention, an optical multiple beam antenna is used to obtain a
sector beam which has constant beam position and beam shape over a wide
frequency band. The sector beam is formed by simultaneously generating and
overlapping a series of selected beams of the optical multiple beam
antenna so that the overlapping results in a sector beam of the desired
shape. Since the antenna used in the invention operates in accordance with
the principles of optics, the individual beam positions of the series of
overlapping beams are fixed in space and are independent of the operating
frequency. In the invention, the sector beam position and beam shape
remain nearly constant over an octave frequency bandwidth. Some examples
of optical multiple beam antennas usable in the invention are a geodesic
lens antenna, a Luneberg lens antenna, a circular folded pillbox and a
Myer trash can scanner.
The shape of the sector beam is controlled in part by the number of the
feeds to the optical multiple beam antenna. Since the sector beam is
formed by overlapping multiple beams, the number of feeds and placement of
them in relation to one another determine the degree of overlapping of the
beams and thus the sector beam size.
In the invention, a phase progression technique is provided to compensate
for ripple. In the phase progression technique, a phasing control is
coupled to the antenna feeds for varying the ripple. By use of the phasing
control, the optical multiple beam antenna may be suitably defocussed or
phase spoiled such that constant beamwidth and constant edge slope are
obtainable.
A power divider is used to feed the optical multiple beam antenna through
the phasing control means and may have weighted outputs for energy
management or other purposes. For example, more weighting can be given to
the beams located just above the horizon and less weighting given to
higher angle beams where less elevation gain is required.
The optical multiple beam antennas usable in the invention typically have
broad beamwidths in the plane orthogonal to the plane of the multiple
beams and an aperture control device may be coupled to the optical
multiple beam antenna to limit this beamwidth as desired. An aperture
control device consisting of an E-plane sectoral horn having a selected
flare angle operates in accordance with the laws of optics and has been
found to be useful for limiting the E-plane beamwidth of a geodesic lens
antenna. The flare angle of the horn is approximately equal to the
beamwidth.
There are two general varieties of optical multiple beam antennas usable in
the invention, perfectly focussing and imperfectly focussing antennas.
Both types meet the purposes of the invention because their beam positions
are not frequency dependent, however they possess somewhat different
operating characteristics. The perfectly focussing multiple beam antenna
is a lens antenna such as the geodesic and Luneberg lenses, and it has
been found that these antennas have sharper beam edge slopes than the
imperfectly focussing antennas, however the individual beam shapes change
slightly with frequency changes. The imperfectly focussing multiple beam
antennas such as a trash can scanner, a folded circular pillbox, or a
constant k lens, produce nearly constant phase fronts. It has been found
that these antennas can be constructed to maintain a constant beam shape
with frequency changes although the beam edge slope is not as steep as
with the perfectly focussing antennas. The imperfectly focussing multiple
beam antennas also tend to have less ripple, although ripple can be
compensated for in the perfectly focussing antennas through the phasing
control.
Typically, the optical multiple beam antenna and other elements of the
invention are capable of use in both the transmission and reception of
electromagnetic energy. For convenience it is customary to refer to such
elements in terms of their functions in the transmission of
electromagnetic energy while understanding that they are also capable of
reception.
The novel features which are believed to be characteristic of the
invention, both as to its structure and method of operation, together with
further purposes and advantages thereof will be better understood from the
following descriptions considered in connection with the accompanying
drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a chart of superimposed (sin X)/X beams to form a sector beam
pattern;
FIG. 2 is a schematic view of a geodesic lens having two feed probes and
the resultant far field beam shapes;
FIGS. 3a and 3b are graphs of beam shapes of a typical Butler beam forming
array showing the frequency dependence of individual and sector beam
shapes;
FIGS. 3c and 3d are graphs of beam shapes of an antenna constructed in
accordance with the invention;
FIG. 4 presents a perspective view of a circular folded pillbox type
antenna usable in the invention;
FIGS. 5a and 5b present the radiation patterns in the E-plane of a geodesic
lens antenna usable in the invention FIG. 5a presents a typical E-plane
pattern where no aperture control is utilized and FIG. 5b presents the
E-plane pattern with an E-plane sectoral, flared horn attached to the
geodesic lens antenna;
FIG. 6 is a schematic view of the radiation pattern of a Luneberg lens
usable in the invention having feeds spaced over 20.degree. of the lens
periphery;
FIG. 7 presents a schematic block diagram of an antenna system constructed
in accordance with the invention;
FIGS. 8a and 8b present a transition technique usable in the invention for
coupling the feed system to a geodesic lens antenna. FIG. 8a shows a
coaxial shorted probe feed while FIG. 8b shows the schematic circuit
equivalent of a feed similar to FIG. 8a;
FIG. 9 presents a perspective view of an antenna constructed in accordance
with the invention wherein a geodesic lens has an E-plane sectoral horn
and is mounted, on a pedestal;
FIG. 10 presents a graph of a radiation pattern of an embodiment of the
invention at one frequency; and
FIG. 11 presents a graph of a radiation pattern of an embodiment of the
invention at twice the frequency of FIG. 10.
DETAILED DESCRIPTION OF THE INVENTION
Referring now to the drawings with more particularly, FIG. 1 presents a
view of overlapped (sin X)/X beams. Without subscribing to any particular
theory of operation, it appears that the mechanics of operation of the
invention are as generally described in the following paragraphs.
A shaped sector beam having a steep beam edge slope can be realized by
overlapping adjacent (sin X)/X type beams. The sector pattern is exact at
the peaks of the constituent (sin X)/X since the neighboring beams have
nulls at these points. This is the basis of the Woodward pattern synthesis
and is shown in FIG. 1. The edge slopes 30 of the sector 31 are determined
primarily by the slope or beamwidth of a single constituent beam. Also,
the number of sample points in the sector beam, hence the fidelity of the
synthesis, is determined by the width of the constituent beams. The
Woodward viewpoint shows how much aperture is required to produce edge
slope. Since the constituent beams are diffraction limited and the edges
of the sector beam have roughly the same slope as the constituent (sin
X)/X beams, the Woodward viewpoint leads to the smallest aperture required
to produce a required beam edge slope. The slope of the pattern is
approximated by the formula:
##EQU1##
where: P=relative power level in dB in the far field .phi.=angle in
degrees
D/.lambda.=aperture size in wavelengths
On the other hand, the edge slope of an optical antenna such as a horn fed
hyperbola or a large, directly radiating, sectoral horn has an edge slope
of the form:
##EQU2##
Where .phi..sub.0 is the beamwidth. This square root relationship produces
gently sloping edges, therefore, the Woodward synthesis produces the
steeper slope. Woodward synthesis is not entirely a convenient algorithm
for synthesis. Since a Butler matrix will produce adjacent (sin X)/X
beams, a narrow band, direct Woodward mechanization can be constructed by
attaching a weighted output to the Butler matrix in a one to one
accordance with the desired far field beam weighting.
The ideal Butler and ideal corporate feed will produce an aperture
distribution which is constant for all frequencies, but such a
distribution would produce a beam which is a function of k sin .theta..
The Butler beam positions and beamwidths will dilate with frequency
causing a broadening of the sector beam and a change in the edge slope.
This pattern "breathes" with frequency, the cause of which is that the
constituent (sin X)/X Butler beams are not fixed in space or fixed in
beamwidth as the frequency changes.
There is a close relationship between a Butler matrix, which is a multiple
beam antenna feed, and an optical multiple beam antenna such as a geodesic
lens or a two dimensional Luneberg lens. These latter antennas may be
considered as being the optical analog to the Butler matrix. Feed points
spaced one half wavelength apart on a geodesic lens with a cosine feed
power pattern will produce (sin X)/X beams as in the Butler matrix.
However, in the geodesic lens, the beam positions are fixed in space and
are determined by the angle of the feed as schematically shown in FIG. 2.
Geodesic lens 40 has feeds 41 and 42 located on its focal curve. From
these feeds, far field beams 43 and 44 are generated respectively. In the
geodesic lens, as in the Luneberg lens, the individual beams such as beams
43 and 44 in FIG. 2, will change beam slope with frequency somewhat, but
since their positions are fixed in space, the sector beam shape, measured
between outer beam centerlines as shown in FIG. 1 by sector 31, is
constant. Only the sector beam edge slope changes with frequency and not
the sector beam width. This characteristic is shown in FIGS. 3a-3d.
In FIG. 3a, the width 50 between constituent beams of sector beam 51
generated by a typical Butler beam forming array is shown. In FIG. 3b, the
frequency of operation has been reduced from that of FIG. 3a and results
in a wider width 52 between constituent beams and a wider sector beam 53
than that of FIG. 3a. Changing the frequency of operation in the opposite
direction yields opposite results, i.e., a narrowing of both widths. In
the invention, an optical multiple beam antenna is used which has fixed
beam positions. A selected number of overlapped beams are simultaneously
generated to form the sector beam in space. The results of changing the
frequency of operation in this antenna are shown in FIGS. 3c and 3d. In
FIG. 3c, the width 54 between constituent beams and the width of sector
beam 55 are shown. In FIG. 3d, the frequency of operation has been reduced
from that of FIG. 3c. The width 56 between the constituent beams remains
the same as width 54 in FIG. 3c and the sector beamwidth 57 remains the
same as the sector width 55 of FIG. 3c, even though the constituent beams
have changed shape somewhat.
Multiple beam antennas which are usable in the invention may be classified
as two general types; perfectly focussing and imperfectly focussing.
Examples of the perfectly focussing type are the geodesic lens antenna and
the Luneberg lens antenna. Both are known in the art, e.g., see Jasik,
Antenna Engineering Handbook, McGraw-Hill, 1961, pgs. 15-3 to 15-10. It
has been found that the perfectly focussing type may be characterized as
having steeper beam slopes than the imperfectly focussing type, however
the slopes change more with frequency than with the imperfectly focussing
type. Also, it has been found that ripple across the sector beam is higher
with a perfectly focussing type antenna.
The imperfectly focussing type multiple beam antennas such as reflectors
and constant k dielectric lenses have nearly constant phase fronts. It has
been found that where an imperfectly focussing multiple beam antenna such
as a circular folded pillbox or a trash can scanner is used, the edge
slope will remain relatively constant with frequency change. However, as
discussed, it has been found that the edge slope is not as great as in the
perfectly focussing multiple beam antennas but there is a decrease in
ripple through the sector beam. A folded circular pillbox type antenna
usable in the invention is shown in FIG. 4. Pillbox 60 has a feed circle
61 centered from point 62. Circular reflector 64, also centered from point
62 but with about twice the radius of feed circle 61, is connected to
waveguide horn 65 and to aperture control 66 which narrows the beam in the
E-plane. A more detailed discussion of a pillbox antenna is located in S.
Silver, Microwave Antenna Theory and Design, Vol. 12, Radiation Laboratory
Series, McGraw-Hill, N.Y., 1949, pgs. 459-464. For a more detailed
description of the trash can scanner, refer to S. B. Meyer, "Journal of
Applied Physics," Vol. 18, 1947, pg. 221.
When using an optical multiple beam antenna such as a geodesic lens in the
invention, the pattern in the plane orthogonal to the plane of the
multiple beams is typically very broad. FIG. 5a shows the radiation
pattern 70 which is typical in a geodesic lens with no aperture control on
the periphery 71. When a more directional pattern is desired, an aperture
control such as horn 72 in FIG. 5b may be coupled to periphery 71. A horn
such as horn 72 is believed to be particularly useful in the invention
since it operates in accordance with the principles of optics. Horn 72 is
a well-known E-plane sectoral horn and is shown reducing the beamwidth in
FIG. 5b, but with gentle edge slope. To sharpen the beam edges, a large
horn would be required since the slope is based on (kD)1/2 in the E-plane,
where k is the wave number and D is the aperture dimension. Other types of
aperture controls may be used in the invention including a line source, a
lens, a shaped offset reflector, or an array.
As was previously discussed, the size of the sector beam of the antenna in
accordance with the invention, depends upon the number and location of the
feeds to the multiple beam antenna. For example, where a sector angle of
20.degree. is desired, feed horns spanning 20.degree. of the periphery of
a Luneberg lens antenna may be used as shown diagrammatically in FIG. 6.
These horns will produce a 20.degree. far field pattern with steep edge
slope. This technique is also applicable to the folded circular pillbox
antenna such as that shown in FIG. 4 where the sector beam angle is
determined by the angle of the feed circle 61 used and the number of horns
used. FIG. 6 show diagrammatically the five feed horns 81-85 are used. The
use of five feed horns is shown for explanation purposes only. It has been
found that feeds spaced at one-half wavelength or less, of the highest
frequency of operation produce a desirable sector beam in the invention.
A shaped beam antenna in accordance with the invention is schematically
shown in FIG. 7 where power divider 90 is feeding a geodesic lens antenna
91 through phasing control device 92 and amplitude weighting device 95.
The signals are coupled to the geodesic lens antenna 91 by feed probes 94.
As discussed, it has been found that feeds spaced from each other by
one-half wavelength or less at the highest frequency of operation create a
sector beam with steep beam edge slopes. Power divider 90 divides the
input signal from feed line 93 into the number of signals corresponding to
the number of feed probes used in the particular embodiment. Where energy
management is a concern, the output signals of power divider 90 may be
amplitude weighted by amplitude weighting device 95. For a pattern where
more energy is to be transmitted to the lower elevation angles than to the
higher elevation angles, proper weighting of power divider outputs can
achieve this pattern. Power dividers usable in the invention include
waveguide types, coaxial line types, stripline, radial line, E-plane
separated waveguide and others known in the art. Amplitude weighting
devices are well known in the art and are not further discussed.
Coupling of the input feeds to the optical multiple beam antenna can be
critical in that frequency bandwidth and power handling capabilities can
be affected. Coupling can be accomplished by using techniques such as a
waveguide transition, a dumb-bell probe, a shorted probe, a loop and
others known in the art. To achieve a focussing of the beams, the fixed
phase center of the feed is placed on the focal curve of the optical
multiple beam antenna. A shorted probe technique applied to a geodesic
lens antenna is shown in FIG. 8a. This technique is suitable for coaxial
inputs such as coax 104 and uses a conventional stepped impedance
transformer 103. For in-phase excitation, one can define a "cell" in the
lens having spacing equal to the probe spacings; the sides may be
considered to be magnetic walls, and top and bottom the electric walls.
The impedance Z.sub.O of this cell is:
##EQU3##
where: a=the probe spacing
s=the plate separation
##EQU4##
A broadband perpendicular transition is shown in FIG. 8a where the probe
100 extends across the spacing between the plates 105 and is shorted at
the bottom 101. A loaded, high impedance 102 is placed on one side and
impedance step 103 is located in the coax 104 and/or in the parallel
plates 105 as shown in FIG. 8a. There are other transitions known to those
skilled in the art which will also function in the invention. However, it
is believed that the design shown in FIG. 8a is of particular practical
importance because it has a distinct frequency independent phase center
located at the opening to the high impedance section 102. FIG. 8b presents
a schematic diagram of the electrical equivalent circuit of a transition
where there is a two step transformer using lines 106 and 107 and an
infinite impendance 108, a 50 ohm impedance input 109, and the parallel
plate impedance at 110. Waveguide coupling is of practical use in the
invention and techniques for the broadband matching of phased array
antennas are applicable to the invention as well. For a more detailed
discussion of transitions, refer to Ragan, Radiation Laboratory Series,
Vol. 9, pgs. 314-405.
Feeding a Luneberg lens antenna such as lens 80 of FIG. 6 is accomplished
by feed means such as truncated waveguides, probes or other feed means
known in the art. Also shown in FIG. 6 is power divider 86, amplitude
weighting device 87, phasing control 88 and aperture control 89.
Phasing control device (88 as shown in FIG. 6 and 92 as shown in FIG. 7),
is used in the invention to control beam ripple. In the Woodward approach,
the correct power is obtained at the sample points regardless of phase
since theoretically only one beam contributes to the outputs at these
points. However practically, interbeam phase shift can be used to control
the pattern ripple at the crossover level of the constituent beams. For
uniformly shaped sectoral beams, it has been found that the ripple away
from the edges is insensitive to the chosen phase progression. Varying the
phase can result in less ripple near the beam edges. Phasing control
devices usable in the invention include posts or buttons in waveguide,
line lengths, shunt stubs in stripline, dielectric slugs and others known
in the art.
FIG. 9 presents a perspective view of an antenna constructed in accordance
with the invention, wherein a geodesic lens antenna 120 is mounted in a
stabilizing pedestal 122. A coaxial feedline 124 enters power divider,
amplitude weighting and phase control devices which are located in a
cabinet 126. The typical contents of the cabinet 126 are shown
schematically in FIG. 7 as power divider 90, amplitude weighting means 95
and phase control means 92. As required, the stabilizing pedestal 122 is a
fixed mounting or a moveable mounting such as where it must compensate for
ship pitch and roll. The aperture horn 128 is a sectoral horn for
narrowing the beam and has a dielectric sheet 130 covering its external
opening for weather protection.
In the antenna shown in FIG. 9, relatively high power levels may be
conducted since the geodesic lens antenna is a parallel plate, air
dielectric lens antenna. The power handling capabilities are critically
affected by the input feed system shown as shorted probe 100 in FIG. 8a. A
design such as that shown in FIG. 8a will result in efficient power
transfer from the feed system to the geodesic lens. Matching of the
geodesic lens to the feed may be accomplished by techniques known to those
skilled in the art. One technique is shown in FIG. 8a where a stepped
plate transformer 103 is used.
Another consideration in the use of a geodesic lens antenna in the
invention is the plate spacing. If the plate spacing is maintained at less
than one half wavelength, and the lens radius is much greater than one
wavelength, then the geodesic lens antenna will function according to
optical theory. Another consideration with any geodesic analog to a
Luneberg lens is the technique for bending the rays which leave the dome
shaped surface. Typically, a toroidal bend is used, however it has been
found that mitered bends (also usable in the circular folded pillbox
antenna) function in accordance with optical theory. Compensation for the
defocusing caused by the introduction of the bends is accomplished by
techniques known to those skilled in the art. For a more detailed
discussion, refer to H. Jasik, Antenna Engineering Handbook, McGraw-Hill,
1961, pgs. 15-6 to 15-8 and R. C. Johnson, "The Geodesic Luneberg Lens",
The Microwave Journal, Aug. 1962, pgs. 76-85.
An embodiment of the invention was built to operate in the 14.5 to 17.0 GHz
frequency band. A waveguide power divider and a geodesic lens which was
fitted with an E-plane sectoral horn were interconnected using coaxial
cables and transitions similar to that discussed above and shown in FIG.
8a. Line lengths were used to control the relative phasing. Patterns
obtained show the steep beam edge slope as predicted as well as the
constant beamwidth instead of the usual proportionality between beamwidth
and wavelength obtained using prior techniques. Edge slope was measured at
12.5 dB/degree in an embodiment using a 96.52 cm (38 inch) geodesic lens
antenna and one half wavelength spaced probes along a 20.degree. arc on
the feed circle. This configuration yielded a beamwidth in the far field
of 19.4.degree., and ripple was measured at .+-.0.3 dB at 14.5 GHz as
shown in FIG. 10. At 17.0 GHz, the ripple increased to .+-.0.8 dB/degree,
the beam width was 19.9 degrees and the edge slope was 13.3 dB/degree as
shown in FIG. 11. A phenomenon noticed in this embodiment was that the
sector beamwidth, measured between the 3 dB points, remained nearly
constant even though the operating frequency was changed by a factor of
approximately 5/4, and the constituent beams changed shape.
Thus, there has been shown and described a new and useful wideband shaped
beam antenna. Rather than attempting to shape a single beam into a sector
beam, the invention provides an overlapped plurality of selected single
beams which form the sector beam. The sector beam edges are, effectively,
the edges of two single beams. The principal advantages of the invention
are the ability to maintain a constant prescribed beam position and beam
shape over an octave frequency bandwidth with steep beam edge slopes in
one plane. The beam edge slope is proportional to kD instead of the less
steep (kD).sup.1/2 relationship common to direct radiating antennas used
in the past. The invention is also capable of handling high power levels.
Since the feed design can be a loaded waveguide, the power levels can be
made extremely high. In the case of a geodesic lens antenna, most of the
transmission path is in air, therefore loss is low. Geodesic lenses are
relatively inexpensive to construct. Beam ripple and edge slope can be
controlled over octave frequency bandwidth by the use of phasing control
at the lens inputs and by using an imperfectly focussing lens.
Although described in a shipboard application with steep beam edges being
placed in the elevation plane, there are other uses both active and
passive, which will benefit from the present invention. Any system which
requires a constant shaped sector beam in one plane and which must operate
over wide frequency bandwidths can employ the present invention. The
characteristic of a wide frequency bandwidth may also make the invention
desirable to an application where the antenna is shared between two or
more narrow frequency band systems having widely separated center
frequencies. This feature may be important to a shipboard application
where lofty antenna sites are scarce and the present antenna could be used
to share two or more communication systems.
Although the invention has been described and illustrated in detail, this
is by way of example only and is not meant to be taken by way of
limitation. Modifications to the above description and illustrations of
the invention may occur to those skilled in the art, however it is the
intention that the scope of the invention should include such
modifications unless specifically limited by the claims.
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